SAE AMS 5662M-2004
自耗电极或真空感应熔炼1775°F (968℃)固溶热处理沉淀硬化的含52.5Ni-19Cr-3.0Mo-5.1Cb (Nb)-0.90Ti-0.50Al-18Fe耐腐蚀和耐热的镍合金棒材,锻件和环件

Nickel Alloy, Corrosion and Heat Resistant, Bars, Forgings, and Rings 52.5Ni 19Cr 3.0Mo 5.1Cb (Nb) 0.90Ti 0.50Al 18Fe, Consumable Electrode or Vacuum Induction Melted 1775°F (968°C) Solution Heat Treated, Precipitation Hardenable

SAE AMS 5662M-2004 发布历史

This specification covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging flash welded rings or heading. These products have been used typically for parts requiring high resistance to creep and stress-rupture up to 1300 degrees F (704 degrees C) and oxidation resistance up to 1800 degrees F (982 degrees C), particularly those parts which are formed or welded and then precipitation heat treated to develop required properties, but usage is not limited to such applications.

SAE AMS 5662M-2004由美国机动车工程师协会 US-SAE 发布于 2004-07-12。

SAE AMS 5662M-2004 在中国标准分类中归属于: V11 航空与航天用金属铸锻材料，在国际标准分类中归属于: 49.025.15 有色金属合金综合。

SAE AMS 5662M-2004 发布之时，引用了标准

• SAE AMS 2261G-2002 
• SAE AMS 2269E-1994 化学检验分析限值,镍,镍合金和钴合金
• SAE AMS 2371G-2003 耐腐蚀耐热的钢和合金锻制品及锻坯的质量保证抽样和试验
• SAE AMS 2374D-2002 
• SAE AMS 2750C-1990 高温测定法

SAE AMS 5662M-2004的历代版本如下：

• 2004年07月12日 SAE AMS 5662M-2004 自耗电极或真空感应熔炼1775°F (968℃)固溶热处理沉淀硬化的含52.5Ni-19Cr-3.0Mo-5.1Cb (Nb)-0.90Ti-0.50Al-18Fe耐腐蚀和耐热的镍合金棒材,锻件和环件

SAE AMS 5662M-2004 洗脸池用金属支架 由 SAE AMS 5662L-2000 变更而来。

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标准号

SAE AMS 5662M-2004

发布日期

2004年07月12日

实施日期

废止日期

无

中国标准分类号

V11

国际标准分类号

49.025.15

发布单位

美国机动车工程师协会

引用标准

ASTM E 8-2004 ASTM E 8M-2004 ASTM E 10-2001 ASTM E 21-2003 ASTM E 103-1984 ASTM E 112-1996 ASTM E 139-2000 ASTM E 292-2001 ASTM E 354-1993 SAE AMS 2261 SAE AMS 2261G-2002 SAE AMS 2269E-1994 SAE AMS 2371G-2003 SAE AMS 2374D-2002 SAE AMS 2750C-1990 SAE AMS

被代替标准

SAE AMS 5662L-2000

适用范围

This specification covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging flash welded rings or heading. These products have been used typically for parts requiring high resistance to creep and stress-rupture up to 1300 degrees F (704 degrees C) and oxidation resistance up to 1800 degrees F (982 degrees C), particularly those parts which are formed or welded and then precipitation heat treated to develop required properties, but usage is not limited to such applications.